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    Shipboard air vehicle retrieval apparatus
    121.
    发明授权
    Shipboard air vehicle retrieval apparatus 失效
    船上空气车辆检索装置

    公开(公告)号：US4753400A

    公开(公告)日：1988-06-28

    申请号：US14314

    申请日：1987-02-13

    Applicant: James D. Reuter ,  Alan H. Greenstadt

    Inventor： James D. Reuter ,  Alan H. Greenstadt

    IPC: B64F1/02

    CPC classification number: B64F1/02 ,  B64C2201/182

    Abstract: A shipboard mounted apparatus for the retrieval of air vehicles, including remotely piloted, or automonous, unmanned vehicles, which includes a deployable lifting device such as a ram-air parachute which is secured through a tow line to the ship traveling upwind therebelow. A capturing device such as a ribbon parachute which may be annular is also movably secured to the tow line immediately below the ram-air parachute and may include a homing beacon therein such that capture of an air vehicle is achieved by it traveling into and collapsing this ribbon parachute. A winch is secured to the ship therebelow and is attached to the lower end of the tow line to control the inward and outward movement of the extended tow line. Once an air vehicle is captured in the ribbon parachute, the tow line is pulled in by the winch allowing the collapsed ribbon parachute and the captured air vehicle to be drawn into the ship to thereby be received by a landing net preferably of an open mesh nylon webbing. An initial launching device can be included such as an additional parachute or an explosive mortar device to provide the initial air-borne impetus to the ram-air parachute and ribbon capturing parachute.

    Abstract translation: 一种用于检索包括遥控或自动无人驾驶车辆在内的机载车辆的船上安装装置，其包括可升降的升降装置，例如冲压空降落伞，该升降装置通过拖绳固定到沿着上游风向的船舶。 诸如可以是环形的带状降落伞的捕获装置也可移动地固定到冲压空气降落伞正下方的拖绳上，并且可以在其中包括归巢信标，使得通过其行进和塌缩来实现空中交通工具的捕获 丝带降落伞。 绞车被固定在其下方的船上，并连接到拖绳的下端以控制延伸的拖绳的向内和向外的运动。 一旦空中飞行器被捕获在带状降落伞中，则牵引线被绞盘牵引，允许收缩的带状降落伞和被捕获的空中车辆被吸入船中，从而被一个着陆网接收，优选地是开式网状尼龙 织带。 可以包括一个初始发射装置，例如附加的降落伞或爆炸性砂浆装置，以便为冲压空降落伞和色带捕获降落伞提供初始的空气动力。

    Arrestment system
    122.
    发明授权
    Arrestment system 失效
    逮捕制度

    公开(公告)号：US4311290A

    公开(公告)日：1982-01-19

    申请号：US90205

    申请日：1979-11-01

    Applicant: Kenneth T. Koper

    Inventor： Kenneth T. Koper

    IPC: B64F1/02

    CPC classification number: B64F1/02 ,  B64C2201/105 ,  B64C2201/107 ,  B64C2201/182 ,  B64C2201/185

    Abstract: Apparatus and method for recovering and arresting an aircraft or other vele. A boom is swivelly connected to a support structure via braking mechanism. The boom is pivotally connected to the brake mechanism such that it can also pivot in a second, different plane intersecting the plane of rotation of the brake mechanism. A shear pin prevents pivoting of the boom in the second plane until the boom has experienced a predetermined load in that plane. The distal end of the boom distant from the brake mechanism is provided with structure for engaging the aircraft. When the aircraft is flown at and captured by the boom, the weight and motion of the aircraft breaks the shear pin, causing the boom to move in the second plane until engaged by a stop. This rapid change in position of the engaging end of the boom in the second plane prevents the aircraft from pendulating about the boom. Forward motion of the aircraft also causes movement within the brake mechanism in the first plane which absorbs the kinetic energy of the aircraft as the boom swivels against the brake mechanism, so that the aircraft is slowed and arrested.

    Abstract translation: 用于恢复和阻止飞机或其他车辆的装置和方法。 动臂通过制动机构旋转地连接到支撑结构。 吊杆枢转地连接到制动机构，使得其也可以在与制动机构的旋转平面相交的第二不同平面中枢转。 剪切销防止悬臂在第二平面中的枢转，直到悬臂在该平面中经历了预定的载荷。 离开制动机构的悬臂的远端设置有用于接合飞行器的结构。 当飞机飞行并被悬臂捕获时，飞行器的重量和运动会破坏剪切销，导致吊臂在第二平面中移动，直到停止。 在第二平面中，起重臂的接合端的这种快速变化防止飞机在吊杆周围摆动。 飞行器的前进运动也引起在第一平面内的制动机构内的运动，当悬臂靠在制动机构上转动时吸收飞行器的动能，从而使飞行器减慢和停止。

    Mobile RPV landing deck
    123.
    发明授权
    Mobile RPV landing deck 失效
    移动RPV登陆甲板

    公开(公告)号：US4147317A

    公开(公告)日：1979-04-03

    申请号：US809478

    申请日：1977-06-23

    Applicant: Harry E. Mayhew ,  Harry W. De Shay

    Inventor： Harry E. Mayhew ,  Harry W. De Shay

    IPC: B64C39/02 ,  B64F1/02

    CPC classification number: B64C39/024 ,  B64F1/02 ,  B64C2201/182

    Abstract: A deck for landing an arrested RPV has a row of substantially parallel elastic stringers deployed between a pair of open bed trailers. The stringers are attached to longitudinal rails on the trailers and to wind-up winches for tensioning the stringers. A pendant or net is attached across one of the trailers between a pair of stanchions and is connected to energy absorbers on the other trailer for arresting the landing RPV and dropping it down on the deck. Protruding elements of the RPV slide down inbetween the stringers to protect them from damage as the larger body and wing portions are caught on the stringers.

    Abstract translation: 用于着陆被捕RPV的甲板在一对敞开式拖车之间具有一排基本平行的弹性桁条。 桁条连接在拖车上的纵向导轨上，并卷起绞车以张紧桁条。 吊坠或网络在一对支柱之间的一个拖车上，并连接到另一拖车上的能量吸收器，用于阻止着陆RPV并将其落在甲板上。 RPV的突出元素在桁条之间向下滑动，以防止它们被损坏，因为较大的身体和翼部分被抓在桁条上。

    TETHERED UNMANNED AERIAL VEHICLE SYSTEM
    124.
    发明申请
    TETHERED UNMANNED AERIAL VEHICLE SYSTEM 审中-公开

    公开(公告)号：US20190002102A1

    公开(公告)日：2019-01-03

    申请号：US16126020

    申请日：2018-09-10

    Applicant: Tribune Broadcasting Company, LLC

    Inventor： Hank J. HUNDEMER

    IPC: B64C39/02 ,  B64F1/02 ,  B64F3/00 ,  B64F3/02

    CPC classification number: B64C39/022 ,  B64C39/024 ,  B64C2201/148 ,  B64C2201/182 ,  B64C2201/208 ,  B64D2201/00 ,  B64F1/02 ,  B64F3/00 ,  B64F3/02

    Abstract: In one aspect, an example system includes: (i) a base including a bottom surface and a first coupling-point; (ii) a vertically-oriented elongate structure comprising a lower end, an upper end, and an inner channel, wherein the inner channel comprises an upper access-point disposed proximate the upper end, wherein the base is coupled to the elongate structure proximate the lower end; (iii) a deployable cushioning-device coupled to the elongate structure; and (iv) a tether comprising a first portion, a second portion, a third portion, and a fourth portion, wherein the first portion is coupled to the first coupling-point, the second portion is coupled to a second coupling-point of the UAV, the third portion extends through the inner channel, the fourth portion extends from the upper access-point to the second coupling-point, and the fourth portion has a length that is less than a distance between the upper access-point and the bottom surface.

    KINETIC UNMANNED AERIAL VEHICLE FLIGHT DISRUPTION AND DISABLING DEVICE, SYSTEM AND ASSOCIATED METHODS
    127.
    发明申请
    KINETIC UNMANNED AERIAL VEHICLE FLIGHT DISRUPTION AND DISABLING DEVICE, SYSTEM AND ASSOCIATED METHODS 审中-公开

    公开(公告)号：US20180257780A1

    公开(公告)日：2018-09-13

    申请号：US15454359

    申请日：2017-03-09

    Applicant: Jeffrey Sassinsky

    Inventor： Jeffrey Sassinsky

    IPC: B64D5/00 ,  B64C39/02 ,  G08G5/00 ,  B64D47/08 ,  B64D7/00 ,  F41H13/00 ,  F41B13/10 ,  F41H9/00 ,  F41H11/02

    CPC classification number: F41H11/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/12 ,  B64C2201/182 ,  B64C2201/206 ,  B64D7/00 ,  B64D47/08 ,  B64F1/02 ,  F41B13/10 ,  F41H9/00 ,  F41H9/04 ,  F41H11/04 ,  F41H13/00 ,  F41H13/0012 ,  F41H13/0062

    Abstract: The present invention is a device, system(s) and/or method(s) for disrupting, capturing, and/or disabling and unmanned aerial vehicle(s) in flight, on the ground, or preparing for flight that may or may not be under the control of the invention operator. In certain embodiments, the invention is supported and carried by an unmanned aerial vehicle that is controlled by a ground operator, a computer process and associate hardware, or any combination thereof. In other embodiments, the invention contains physical destruction devices such as projectiles, explosives, spikes, electric shock generators, etc. The invention is manipulated to track, intercept, capture, disrupt, disable and/or move a target unmanned aerial vehicle. In certain embodiments, the invention includes materials able to contain, at least in part, hazardous materials and/or conditions caused by the target unmanned aerial vehicle. In certain embodiments, the invention interfaces with external unmanned aerial vehicle detection/tracking systems. A unique design element in certain embodiments is the ability to limit the potential of the captured aerial vehicle escaping the device and/or falling to the ground. Another unique design element in certain embodiments is the ability of the invention to limit collateral damage caused by the captured unmanned aerial vehicle or apparatuses contained thereon. Another unique design element is the ability of the invention to interface with external unmanned aerial vehicle detection/tracking systems.

    INTELLIGENT DOCKING SYSTEM WITH AUTOMATED STOWAGE FOR UAVS
    129.
    发明申请
    INTELLIGENT DOCKING SYSTEM WITH AUTOMATED STOWAGE FOR UAVS 审中-公开

    公开(公告)号：US20180134412A1

    公开(公告)日：2018-05-17

    申请号：US15566603

    申请日：2016-04-29

    Applicant: Chung Kiak POH ,  Chung How POH

    Inventor： Chung Kiak POH ,  Chung How POH

    IPC: B64F1/12 ,  B64C39/02 ,  H02S20/30

    CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/084 ,  B64C2201/182 ,  B64C2201/201 ,  B64F1/02 ,  B64F1/222 ,  H02S20/30

    Abstract: The present invention generally relates to a system and method of a docking system (1) for fixed wing unmanned aerial vehicle, or non-fixed wing unmanned aerial vehicle (2) such as rotorcraft, or combination thereof, comprising at least a docking and/or launching pad capable of being arranged in an array or staggered manner; said pad has a surface (6) for said vehicle docking and launching, said docking and launching surface (6) comprising moveable pads (31) which include electromagnets that can be energized to capture a docking vehicle (2); and another energy harvesting surface (4) has photovoltaic panel to harness solar energy to generate electricity or hydrogen fuel for a variety of on-board applications such as to charge said vehicle (2) and to power the docking system and providing a safe stowage and protected storage for the said vehicle (2).

    Utilizing an unmanned aerial vehicle platform which is equipped with a turntable assembly
    130.
    发明授权
    Utilizing an unmanned aerial vehicle platform which is equipped with a turntable assembly 有权

    公开(公告)号：US09957064B2

    公开(公告)日：2018-05-01

    申请号：US14707424

    申请日：2015-05-08

    Applicant: AAI Corporation

    Inventor： Stephen W. Miller ,  Zachary J. Smith ,  Peter J. Helman

    IPC: B64F1/06 ,  B64F1/02 ,  B64C39/02

    CPC classification number: B64F1/06 ,  B64C39/024 ,  B64C2201/084 ,  B64C2201/182 ,  B64F1/02 ,  B64F1/025

    Abstract: An unmanned aerial vehicle (UAV) platform includes a stationary base constructed and arranged to reside over a fixed location on a surface (e.g., a ground location, a ship's deck, a trailer or other vehicle, etc.). The UAV platform further includes a set of UAV interfaces constructed and arranged to interface directly with a UAV (e.g., a launcher, a net apparatus, etc.). The UAV platform further includes a turntable assembly which couples to the stationary base. The turntable assembly is constructed and arranged to couple to each UAV interface and control angular direction of that UAV interface over the fixed location. A method of operating a UAV platform includes deploying the UAV platform over a fixed location, preparing a UAV interface on a turntable assembly of the UAV platform, and rotating the turntable to control angular direction of the UAV interface over the fixed location.

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